Airframe Structural Components: 16T4670-11, 16T4672-16, 16T7200-25
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16T4670-11 16T467011 | 1560-01-115-2780 | Skin, Aircraft | Overall Length: 24.000 inches nominal Overall Width: 6.000 inches nominal Thickness: 0.020 inches nominal | Lockheed Martin Corporation (81755) | |
| 16T4670-7 16T46707 | 1560-01-104-0277 | Skin, Aircraft | III End Item Identification: Acft model F-16 Special Features: Aluminum alloy per QQ-A-250/4-T62, 24.000 in. lg, 19.000 in. W, 0.020 in. thk | Israel Aircraft Industries LTD (1BG25) Lockheed Martin Corporation (81755) Sonaca SA (B0128) | |
| 16T4670-9 16T46709 | 1560-01-104-0278 | Skin, Aircraft | III End Item Identification: F-16 Material: Aluminum alloy Material Document and Classification: QQ-A-250/4-T62 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16T4672-15 16T467215 | 1560-01-081-3967 | Door, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4-T81 fed spec single material response Securing Device Type: Hinge | Lockheed Martin Corporation (81755) | |
| 16T4672-16 16T467216 | 1560-01-081-3968 | Door, Access, Aircraft | Cross-Sectional Shape Style: Arched Width: 6.330 inches nominal Peripheral Shape Style: Rectangle, multi holes | Lockheed Martin Corporation (81755) | |
| 16T4673-9 16T46739 | 1560-01-104-0233 | Frame, Access Hole, Aircraft | Aircraft Mission Design Series: F-16 Material: Aluminum alloy Aircraft Location: Aft chute compartment | Lockheed Martin Corporation (81755) | |
| 16T4674-11 16T467411 | 1560-01-316-7457 | Hinge | Lockheed Martin Corporation (81755) | ||
| 16T4674-7 16T46747 | 1560-01-081-3967 | Door, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4-T81 fed spec single material response Securing Device Type: Hinge | Lockheed Martin Corporation (81755) | |
| 16T4674-8 16T46748 | 1560-01-081-3968 | Door, Access, Aircraft | Cross-Sectional Shape Style: Arched Width: 6.330 inches nominal Peripheral Shape Style: Rectangle, multi holes | Lockheed Martin Corporation (81755) | |
| 16T4674-8S 16T46748S | 1560-01-081-3968 | Door, Access, Aircraft | Cross-Sectional Shape Style: Arched Width: 6.330 inches nominal Peripheral Shape Style: Rectangle, multi holes | Lockheed Martin Corporation (81755) | |
| 16T4675-3 16T46753 | 1560-01-082-4731 | Bracket Assembly, Rudder Fairing | III End Item Identification: Acft model F-16A&B General Characteristics Item Description: C/O bracket P/N 16T4675-9 material per FMS-3002-T851, stock size 2.000 in. thk, 4.000 in. W, 5.000 in. lg, bushing P/N NAS77B4-20N, bushing P/N NAS77B6-20N | Lockheed Martin Corporation (81755) | |
| 16T5884-3 16T58843 | 1560-01-104-0227 | Scoop, Aircraft | Aircraft Mission Design Series: F-16 Special Features: C/O flange P/N 16T5884-9, flange P/N 16T5884-11, duct halfp/N 16T5884-13, duct half P/N 16T5884-14 | Lockheed Martin Corporation (81755) | |
| 16T6241-15 16T624115 | 1560-01-276-7219 | Support, Structural Component, Air | III End Item Identification: F-16A aircraft III Supplementary Features: Functional description:frame assy for forward dorsal fairing | Lockheed Martin Corporation (81755) | |
| 16T6241-3 16T62413 | 1560-01-277-2034 | Support, Structural Component, Air | III End Item Identification: F-16A aircraft III Supplementary Features: Functional description:frame assy, fairing, fwd dorsal | Lockheed Martin Corporation (81755) | |
| 16T6243-1 16T62431 | 1560-01-292-9017 | Leading Edge, Aircraft | Aircraft Mission Design Series: F-16A Aircraft Location: Fwd dorsal leading edge fairing | Lockheed Martin Corporation (81755) | |
| 16T6252-1 16T62521 | 1560-01-293-0224 | Fairing, Aircraft | Aircraft Mission Design Series: F-16A Aircraft Location: Vertical stabilizer root fiting | Lockheed Martin Corporation (81755) | |
| 16T6252-2 16T62522 | 1560-01-293-0225 | Fairing, Aircraft | Aircraft Mission Design Series: F-16A Aircraft Location: Vert stabilizer root fitting | Lockheed Martin Corporation (81755) | |
| 16T6252-3 16T62523 | 1560-01-293-0224 | Fairing, Aircraft | Aircraft Mission Design Series: F-16A Aircraft Location: Vertical stabilizer root fiting | Lockheed Martin Corporation (81755) | |
| 16T6252-4 16T62524 | 1560-01-293-0225 | Fairing, Aircraft | Aircraft Mission Design Series: F-16A Aircraft Location: Vert stabilizer root fitting | Lockheed Martin Corporation (81755) | |
| 16T7200-25 16T720025 | 1560-01-051-2985 | Stabilizer, Vertical | Aircraft Mission Design Series: F-16A/B Special Features: Replaces P/N 16T7200-31, I/C codeom, eff 0007-0027, ecn 53040, nha : 16T7200-825 | Lockheed Martin Corporation (81755) | |
| 16T7200-25 16T720025 | 1560-01-114-7285 | Stabilizer, Vertical | Aircraft Mission Design Series: F-16A/B Special Features: Nha 16T7200-855, superseds 16T7200-39, I/C code ni, eff 61 0293 9999, ecn 97653 | Lockheed Martin Corporation (81755) |